US3929467A - Grain refining of metals and alloys - Google Patents
Grain refining of metals and alloys Download PDFInfo
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- US3929467A US3929467A US362521A US36252173A US3929467A US 3929467 A US3929467 A US 3929467A US 362521 A US362521 A US 362521A US 36252173 A US36252173 A US 36252173A US 3929467 A US3929467 A US 3929467A
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- 229910045601 alloy Inorganic materials 0.000 title claims abstract description 52
- 239000000956 alloy Substances 0.000 title claims abstract description 52
- 238000007670 refining Methods 0.000 title claims abstract description 14
- 229910052751 metal Inorganic materials 0.000 title claims description 17
- 239000002184 metal Substances 0.000 title claims description 17
- 150000002739 metals Chemical class 0.000 title description 4
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims abstract description 72
- 239000000654 additive Substances 0.000 claims abstract description 38
- 229910052759 nickel Inorganic materials 0.000 claims abstract description 37
- 230000000996 additive effect Effects 0.000 claims abstract description 30
- 239000002245 particle Substances 0.000 claims abstract description 28
- QGLKJKCYBOYXKC-UHFFFAOYSA-N nonaoxidotritungsten Chemical compound O=[W]1(=O)O[W](=O)(=O)O[W](=O)(=O)O1 QGLKJKCYBOYXKC-UHFFFAOYSA-N 0.000 claims abstract description 22
- 229910001930 tungsten oxide Inorganic materials 0.000 claims abstract description 22
- 239000000155 melt Substances 0.000 claims description 36
- 238000000034 method Methods 0.000 claims description 32
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 24
- 229910052721 tungsten Inorganic materials 0.000 claims description 22
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 claims description 21
- 239000010937 tungsten Substances 0.000 claims description 21
- 230000003647 oxidation Effects 0.000 claims description 15
- 238000007254 oxidation reaction Methods 0.000 claims description 15
- 229910052804 chromium Inorganic materials 0.000 claims description 14
- 239000011651 chromium Substances 0.000 claims description 14
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 13
- 229910052742 iron Inorganic materials 0.000 claims description 12
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 10
- 229910001080 W alloy Inorganic materials 0.000 claims description 10
- 229910052802 copper Inorganic materials 0.000 claims description 10
- 239000010949 copper Substances 0.000 claims description 10
- 239000000203 mixture Substances 0.000 claims description 10
- 229910052796 boron Inorganic materials 0.000 claims description 9
- 229910017052 cobalt Inorganic materials 0.000 claims description 9
- 239000010941 cobalt Substances 0.000 claims description 9
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 claims description 9
- 239000010936 titanium Substances 0.000 claims description 9
- 229910052719 titanium Inorganic materials 0.000 claims description 9
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims description 8
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 8
- 229910052782 aluminium Inorganic materials 0.000 claims description 8
- 229910052750 molybdenum Inorganic materials 0.000 claims description 8
- MOWMLACGTDMJRV-UHFFFAOYSA-N nickel tungsten Chemical compound [Ni].[W] MOWMLACGTDMJRV-UHFFFAOYSA-N 0.000 claims description 8
- 229910052758 niobium Inorganic materials 0.000 claims description 8
- 239000010955 niobium Substances 0.000 claims description 8
- 229910052726 zirconium Inorganic materials 0.000 claims description 8
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims description 7
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 claims description 7
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 7
- 229910052735 hafnium Inorganic materials 0.000 claims description 7
- VBJZVLUMGGDVMO-UHFFFAOYSA-N hafnium atom Chemical compound [Hf] VBJZVLUMGGDVMO-UHFFFAOYSA-N 0.000 claims description 7
- 238000010438 heat treatment Methods 0.000 claims description 7
- 239000011733 molybdenum Substances 0.000 claims description 7
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 claims description 7
- 229910052715 tantalum Inorganic materials 0.000 claims description 7
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 claims description 7
- 229910052720 vanadium Inorganic materials 0.000 claims description 7
- 238000007711 solidification Methods 0.000 claims description 6
- 230000008023 solidification Effects 0.000 claims description 6
- 229910052799 carbon Inorganic materials 0.000 claims description 4
- 239000007787 solid Substances 0.000 claims description 4
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 3
- 239000011248 coating agent Substances 0.000 claims description 3
- 238000000576 coating method Methods 0.000 claims description 3
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 claims 2
- 229910000601 superalloy Inorganic materials 0.000 abstract description 8
- 238000005266 casting Methods 0.000 description 6
- GPPXJZIENCGNKB-UHFFFAOYSA-N vanadium Chemical compound [V]#[V] GPPXJZIENCGNKB-UHFFFAOYSA-N 0.000 description 5
- 230000001590 oxidative effect Effects 0.000 description 3
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 2
- VEXZGXHMUGYJMC-UHFFFAOYSA-N Hydrochloric acid Chemical compound Cl VEXZGXHMUGYJMC-UHFFFAOYSA-N 0.000 description 2
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 2
- 230000008901 benefit Effects 0.000 description 2
- 230000001680 brushing effect Effects 0.000 description 2
- 239000004148 curcumin Substances 0.000 description 2
- 230000007423 decrease Effects 0.000 description 2
- 230000001419 dependent effect Effects 0.000 description 2
- 239000011888 foil Substances 0.000 description 2
- 239000011159 matrix material Substances 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 229910000480 nickel oxide Inorganic materials 0.000 description 2
- USPVIMZDBBWXGM-UHFFFAOYSA-N nickel;oxotungsten Chemical compound [Ni].[W]=O USPVIMZDBBWXGM-UHFFFAOYSA-N 0.000 description 2
- 230000006911 nucleation Effects 0.000 description 2
- 238000010899 nucleation Methods 0.000 description 2
- GNRSAWUEBMWBQH-UHFFFAOYSA-N oxonickel Chemical compound [Ni]=O GNRSAWUEBMWBQH-UHFFFAOYSA-N 0.000 description 2
- 238000005554 pickling Methods 0.000 description 2
- 239000010935 stainless steel Substances 0.000 description 2
- 229910001220 stainless steel Inorganic materials 0.000 description 2
- -1 0.5 to 5% titanium Chemical compound 0.000 description 1
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 229910001369 Brass Inorganic materials 0.000 description 1
- 241000288673 Chiroptera Species 0.000 description 1
- 229910000570 Cupronickel Inorganic materials 0.000 description 1
- 229910001030 Iron–nickel alloy Inorganic materials 0.000 description 1
- 229910001240 Maraging steel Inorganic materials 0.000 description 1
- 229910017709 Ni Co Inorganic materials 0.000 description 1
- 241001275902 Parabramis pekinensis Species 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 1
- VDGMIGHRDCJLMN-UHFFFAOYSA-N [Cu].[Co].[Ni] Chemical compound [Cu].[Co].[Ni] VDGMIGHRDCJLMN-UHFFFAOYSA-N 0.000 description 1
- JRBRVDCKNXZZGH-UHFFFAOYSA-N alumane;copper Chemical compound [AlH3].[Cu] JRBRVDCKNXZZGH-UHFFFAOYSA-N 0.000 description 1
- 239000010951 brass Substances 0.000 description 1
- 239000001569 carbon dioxide Substances 0.000 description 1
- 229910002092 carbon dioxide Inorganic materials 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- RYTYSMSQNNBZDP-UHFFFAOYSA-N cobalt copper Chemical compound [Co].[Cu] RYTYSMSQNNBZDP-UHFFFAOYSA-N 0.000 description 1
- 238000005097 cold rolling Methods 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- IYRDVAUFQZOLSB-UHFFFAOYSA-N copper iron Chemical compound [Fe].[Cu] IYRDVAUFQZOLSB-UHFFFAOYSA-N 0.000 description 1
- GOECOOJIPSGIIV-UHFFFAOYSA-N copper iron nickel Chemical compound [Fe].[Ni].[Cu] GOECOOJIPSGIIV-UHFFFAOYSA-N 0.000 description 1
- YOCUPQPZWBBYIX-UHFFFAOYSA-N copper nickel Chemical compound [Ni].[Cu] YOCUPQPZWBBYIX-UHFFFAOYSA-N 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 230000001627 detrimental effect Effects 0.000 description 1
- KZHJGOXRZJKJNY-UHFFFAOYSA-N dioxosilane;oxo(oxoalumanyloxy)alumane Chemical compound O=[Si]=O.O=[Si]=O.O=[Al]O[Al]=O.O=[Al]O[Al]=O.O=[Al]O[Al]=O KZHJGOXRZJKJNY-UHFFFAOYSA-N 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 229910001651 emery Inorganic materials 0.000 description 1
- 238000010348 incorporation Methods 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 238000005495 investment casting Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 229910044991 metal oxide Inorganic materials 0.000 description 1
- 150000004706 metal oxides Chemical class 0.000 description 1
- 229910052863 mullite Inorganic materials 0.000 description 1
- 239000002667 nucleating agent Substances 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 238000007528 sand casting Methods 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 239000000377 silicon dioxide Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 229910052725 zinc Inorganic materials 0.000 description 1
- 239000011701 zinc Substances 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/06—Making non-ferrous alloys with the use of special agents for refining or deoxidising
Definitions
- innoculants consisting of internally oxidized copper-nickel, copper-cobalt, copper-nickel-cobalt, copper-iron and copper-iron-nickel alloys, the nickel, cobalt and iron oxidizing preferentially to the copper and acting as the grain refining nuclei.
- nucleating oxide particles be less than 1 micron nn) in size, though particles up to two microns might be used. This followed from the fact that in general the smaller the oxide particle size the greater is the degree of grain refining in the melt. This, however, desirable though it be, gives rise to attendant difficulties for it is both difficult and expensive to prepare additives containing, for example, nickel oxide particles smaller than 1 pm. Too, the presence of copper in some alloys is undesirable, if not actually detrimental. Furthermore, subsequent investigation reflected that the grain refining effect of the copper-containing additives was not as pronounced in respect of thicker section castings.
- the present invention provides a process for grain refining a metal or alloy during solidification from the molten state by introducing to a melt of the metal or alloy at least a small but effective amount of a grain refining additive comprised of a nickel carrier and tungsten oxide particles preferably formed by internal oxidation, so that the nickel dissolves and solid tungsten oxide nuclei are introduced into the melt, the
- oxide particles not being restricted to sizes of less than 1 pm as a practical matter.
- a particle size of up to at least 2 pm can be used quite satisfactorily.
- a nickeltungsten alloy To form the additive by internal oxidation a nickeltungsten alloy must be used. While a wide range of nickel-tungsten alloys can be utilized, the size of the oxide particles formed is dependent on the alloy composition. Thus, as the tungsten content of the alloys increases, the rate of internal oxidation decreases and the size of the oxide particles formed tends to become larger. in this connection, it might be said that the larger a given size does mean a smaller ratio of oxide particles to nickel carrier strip and this could add to cost. For such reasons the tungsten content of the alloy should not exceed 17% and more advantageously should not exceed 6%.
- the alloy contains at least 1% of tungsten and more preferably at least 3%.
- the nickel-tungsten alloy should preferably be single-phased since in a two-phased alloy the second phase may enter the melt as undissolved particles which, while not necessarily harmful, could nonetheless interfere with the nucleation of grains.
- the efficiency of nucleation is found to fall off as the temperature of the melt rises, and in treating nickel-based alloys particularly the temperature of the melt preferably should not exceed about 1500C. and more beneficially should not exceed about 1470C.
- the internal oxidation of the alloy to obtain the oxide nuclei is most conveniently effected by heating the alloy in air, although other atmospheres such as carbon dioxide can be used. It is preferable, in order to obtain as many oxide nuclei as possible, to-carry out the oxidation process for a period sufficient such that the alloy is internally oxidized virtually right through the center. However, to avoid excessive scaling losses, the heating should be stopped once the desired oxidation has been achieved. We have found that scaling losses are reduced if the oxidation process in air is continued to the point that an external article coating is formed and the remainder of the oxidation process is conducted in a substantial vacuum. This particularly applies to nickeltungsten alloys containing less than about 10% tungsten. The alloy may become oxidized externally as well as internally. It is of advantage that surplus oxide be removed as by brushing or pickling, before the additive is introduced into the melt. The additive may also advantageously be degreased before use.
- Additives containing tungsten oxide particles are particularly useful in the grain refining of a wide range of melts of alloys containing nickel, such as alloys having as their base nickel and copper or nickel and chromium or nickel, chromium and cobalt, in each case with or without iron up to 50%.
- Such alloys include those which have a base composed of from 20 to 80% nickel, to 35% chromium, 0 to 40% cobalt and 0 to 50% iron, and which may also contain one or more of the elements such as aluminum or titanium up to each, and molybdenum, niobium, tantalum, tungsten, vanadium, zirconium, boron and hafnium in the amounts commonly present in high temperature alloys, e.g., up to molybdenum, up to 8% of niobium and/or tantalum, up to 25% tungsten, up to 3% vanadium, up to 2% zirconium, up to 0.5 or 1% boron (preferably less than 0.1% boron), and up to 5% hafnium.
- a base composed of from 20 to 80% nickel, to 35% chromium, 0 to 40% cobalt and 0 to 50% iron
- Such alloys include those which have a base composed of from 20 to 80% nickel, to 35%
- the additive may also be useful for treating melts which are refined and cast at lower temperatures, for example, melts of copper-aluminum alloys, stainless steel and other alloy steels, and brasses, e.g., 70% copper-30% zinc brass.
- Ni-2%W and Ni-4%W alloys were heated at 1140C. and the Ni-l5%W alloy at 1200C. In each case the heating was continued for four hours, but with the 2% and the 4% tungsten alloys the air was removed after minutes and the heating completed in vacuum and this minimized scaling losses.
- the vacuum technique was unsuitable for the Ni-15%W alloy since the internal oxidation proceeded extremely slowly.
- the predominant composition of the additives thus prepared was Ni-3% tungsten oxide for the additive made from the alloy containing 2% tungsten, Ni-5% tungsten oxide for the additive made from the alloy containing 4% tungsten and Ni-19% tungsten oxide for the additive made from the alloy containing 15% tungsten.
- the average size of the oxide particles was 0.2 pm, 0.4 pm and 1.5 pm, respectively.
- the oxidized strip was quenched into water, and surface oxide film removed by rubbing with emery paper, or by scratch brushing, preferably after coldrolling slightly to fracture the scale, or by pickling, for example, in hydrochloric acid.
- melts of this alloy An additive in the form of the strip prepared as described above and attached to a silica stirrer was introduced into melts of this alloy.
- the melts were poured into sythetic mullite molds (2.8 inches in diameter, 7.5 inches high, 1 inch wall thickness) preheated to 800 to 1000C. and a hot-topping compound was then added, the melts being allowed to solidify.
- the extent of grain refinement was determined by comparing the as-cast structure of a transverse section of the inoculated ingots with that of a similar section taken from an untreated ingot otherwise prepared in the same fashion. The sections were taken from a position mid-way between the bottom of the shrinkage pipe and the bottom of the ingot avoiding columnar crystals grown from the bottom.
- TABLE I Tungsten Oxide The following was used to classify the ingot structures:
- E medium equiaxial grain 2.5 to 4.5 mm. diameter C,, medium columnar grain; 2.5 to 4.5 mm. diameter
- E coarse equiaxial grain 4.5 to 6.0 mm. diameter C coarse columnar grain; 4.5 to 6.0 mm. diameter C very coarse columnar grain; mm. diameter
- the alloy used to produce the wheel was of the nickel-base superalloy type and was of the following approximate composition: 0.05%C, 11.75%Cr, 4.5%Mo, 6%Al, 0.7%Ti 2%Nb, 0.01%B, 0.1%Zr, balance nickel.
- the alloy was vacuum melted and cast in investment shell molds preheated to 800C. with a metal temperature of 1460C.
- the wheel was cut in half to show the grain size in the hub as well as the blade. The grain size was uniform throughout both sections, being less than about 1/16 inch in the hub.
- a similar wheel was cast without aid of the innoculant and the grain size in the hub was 'approximately A to inch, approximately 4 to 8 times larger.
- the subject invention has been used to grain refine a 25%Cr-20%Ni stainless steel and an 18%Ni maraging steel. It is considered that copper base alloys can be grain refined.
- the process of the invention can be used both in the casting of ingots and in the production of castings, i.e., articles and parts made by casting.
- the castings may be made by investment casting in vacuum, air or an inert atmosphere, or by conventional sand casting methods.
- tungsten oxide While the oxide formed by internal oxidations of nickel-tungsten alloys is referred to in this specification as tungsten oxide, it is suspected that in practice the oxidation of such alloys may lead to additives containing some amount of nickel oxide. In-other words, a mixed oxide, for example, NiO W0 may be dispersed in the nickel carrier. Irrespective of this, the actual tungsten oxide content should preferably be from 1 or 2 to 8%.
- a process for grain refining a metal or alloy during solidification from the molten state which comprises introducing into a melt of the metal or alloy an in- I noculating additive comprised of a nickel carrier and tungsten oxide particles in at least a small but effective amount sufficient to induce grain refinement upon solidification, nickel dissolving in the melt and solid tungsten oxide nuclei being dispersed therein.
- melt is an alloy with a base of nickel or nickel and copper or nickel and chromium or nickel, chromium and cobalt, in each case with or without iron up to 50%.
- melt is an alloy having a composition falling within the following ranges: 20 to nickel, 5 to 35% chromium, 0 to 40% cobalt and 0 to 50% iron, up to 10% aluminum, up to 10% titanium, up to 15% molybdenum, up to 8% niobium, up to 8% tantalum, up to 25% tungsten, up to 3% vanadium, up to 2% zirconium, up to 1% boron and up to 5% hafnium.
- melt is an alloy having a composition falling within the following ranges: from 6% to 30% chromium, up to 30% iron, aluminum in an amount of at least 0.4 to 8%, up to 6% titanium, up to 8% molybdenum, up to 20% tungsten, up to 0.25% carbon, upto 6% niobium, up to 6% tantalum, up to 3% vanadium, up to 0.5% boron, up to 2% zirconium, up to 5% hafnium, and at least about 50% nickel.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Manufacture And Refinement Of Metals (AREA)
Abstract
An innoculating additive comprised of a nickel carrier and tungsten oxide particles is useful in grain refining alloys such as nickel-base superalloys.
Description
Davies et al.
GRAIN REFINING OF METALS AND ALLOYS Inventors: Peter Wesley Davies; John Philip Dennison, both of Swansea, England Assignee: The International Nickel Company,
Inc., New York, N.Y.
Filed: May 21, 1973 Appl. No.: 362,521
References Cited UNITED STATES PATENTS 12/1917 Ladoff 75/93 G 8/1927 l/1940 1/1940 7/1971 l/l972 10/1973 51 Dec. 30, 1975 De Bats 75/93 G Mansfield 75/138 Mansfield 75/138 X Lambert et al. 75/171 X Davies et a1. 75/135 Metz 75/129 X Primary ExaminerAl1en B. Curtis Assistant Examiner-Thomas A. Waltz Attorney, Agent, or Firm-Raymond J. Kenny; Ewan C. MacQueen ABSTRACT An innoculating additive comprised of a nickel carrier and tungsten oxide particles is useful in grain refining alloys such as nickel-base superalloys.
11 Claims, N0 Drawings GRAIN REFINI NG OF METALS AND ALLOYS The subject invention is addressed to the grain refinement of metals and alloys, particularly nickel-base superalloys, during the process of solidification from the molten state. i
As the metallurgist is aware, reduction in the grain size of a metal or alloy can be effected if solid particles which act as nuclei are added to a molten bath of the metal to be cast. To that end, in our United Kingdom patent specification 1,239,066 we advanced the concept of incorporating in a molten metal matrix a grain refining nucleating additive consisting of particles of metal oxide dispersed in a carrier metal, the additive having been formed by internal oxidation of an alloy. Upon being introduced into'the melt the metal carrier dissolves, the oxide particles being left as a fine dispersion in the melt matrix. We specifically proposed the use of innoculants consisting of internally oxidized copper-nickel, copper-cobalt, copper-nickel-cobalt, copper-iron and copper-iron-nickel alloys, the nickel, cobalt and iron oxidizing preferentially to the copper and acting as the grain refining nuclei.
We further deemed it most preferable that nucleating oxide particles be less than 1 micron nn) in size, though particles up to two microns might be used. This followed from the fact that in general the smaller the oxide particle size the greater is the degree of grain refining in the melt. This, however, desirable though it be, gives rise to attendant difficulties for it is both difficult and expensive to prepare additives containing, for example, nickel oxide particles smaller than 1 pm. Too, the presence of copper in some alloys is undesirable, if not actually detrimental. Furthermore, subsequent investigation reflected that the grain refining effect of the copper-containing additives was not as pronounced in respect of thicker section castings.
In. any case, it has now been found unexpectedly that if instead of nickel, cobalt or iron the preferentially oxidized metal is tungsten and that nickel as opposed to copper is the carrier metal, then the degree of grain refinement obtained by this special combination is not dependent to the same extent on oxide particle size. This obviates the need for oxide particles of very small size. And, of course, recourse to a copper carrier is eliminated. It might be mentioned that copper is seldom, if ever, an intentionally added constituent in nickelbase superalloys.
Furthermore, it was also found that when using tungsten oxide particles in very slowly cooled ingots, substantially better grain refinement was experienced than by the use of any other tested oxide particles. This lends markedly to producing thick section castings. Indeed, an integrally precision cast nickel-base superalloy turbine wheel, i.e., blade and hub, has been prepared using tungsten oxide as the innoculant on a nickel strip carrier and the grain size in the hub was actually as fine as that in the blade. Insofar as we are aware, this has never been accomplished heretofore, at least by the incorporation of a nucleating agent.
Accordingly, the present invention provides a process for grain refining a metal or alloy during solidification from the molten state by introducing to a melt of the metal or alloy at least a small but effective amount of a grain refining additive comprised of a nickel carrier and tungsten oxide particles preferably formed by internal oxidation, so that the nickel dissolves and solid tungsten oxide nuclei are introduced into the melt, the
oxide particles not being restricted to sizes of less than 1 pm as a practical matter. A particle size of up to at least 2 pm can be used quite satisfactorily.
To form the additive by internal oxidation a nickeltungsten alloy must be used. While a wide range of nickel-tungsten alloys can be utilized, the size of the oxide particles formed is dependent on the alloy composition. Thus, as the tungsten content of the alloys increases, the rate of internal oxidation decreases and the size of the oxide particles formed tends to become larger. in this connection, it might be said that the larger a given size does mean a smaller ratio of oxide particles to nickel carrier strip and this could add to cost. For such reasons the tungsten content of the alloy should not exceed 17% and more advantageously should not exceed 6%. On the other hand, should the tungsten content be too low, the number of particles formed by oxidizing a given weight of the alloy decreases, so that an excessive amount of the carrier needs to be introduced. It is therefore preferred that the alloy contains at least 1% of tungsten and more preferably at least 3%.
The nickel-tungsten alloy should preferably be single-phased since in a two-phased alloy the second phase may enter the melt as undissolved particles which, while not necessarily harmful, could nonetheless interfere with the nucleation of grains. The efficiency of nucleation is found to fall off as the temperature of the melt rises, and in treating nickel-based alloys particularly the temperature of the melt preferably should not exceed about 1500C. and more beneficially should not exceed about 1470C.
The internal oxidation of the alloy to obtain the oxide nuclei is most conveniently effected by heating the alloy in air, although other atmospheres such as carbon dioxide can be used. It is preferable, in order to obtain as many oxide nuclei as possible, to-carry out the oxidation process for a period sufficient such that the alloy is internally oxidized virtually right through the center. However, to avoid excessive scaling losses, the heating should be stopped once the desired oxidation has been achieved. We have found that scaling losses are reduced if the oxidation process in air is continued to the point that an external article coating is formed and the remainder of the oxidation process is conducted in a substantial vacuum. This particularly applies to nickeltungsten alloys containing less than about 10% tungsten. The alloy may become oxidized externally as well as internally. It is of advantage that surplus oxide be removed as by brushing or pickling, before the additive is introduced into the melt. The additive may also advantageously be degreased before use.
To ensure that the nuclei become uniformly dispersed throughout the melt, it is important to prevent local chilling of the melt when the additive is introduced. For this reason, it is advantageous to use additives which have a small cross section, and it is particularly advantageous to use strip or foil from 0.05 to 0.4 mm. in thickness. Another reason for using such foil is that the depth of penetration of the internal oxidation is a function of time and temperature, so that an alloy of greater thickness requires a longer time at the oxidizing temperature if it is to be fully internally oxidized. With a fully internally oxidized alloy, as little as 0.1% additive by weight of the melt would introduce sufficient nuclei to be effective in refining the grains, but in general from about 0.2 or 0.3 to 0.5 or 0.8% of additive by weight of the melt is a suitable addition.
Additives containing tungsten oxide particles are particularly useful in the grain refining of a wide range of melts of alloys containing nickel, such as alloys having as their base nickel and copper or nickel and chromium or nickel, chromium and cobalt, in each case with or without iron up to 50%. Such alloys include those which have a base composed of from 20 to 80% nickel, to 35% chromium, 0 to 40% cobalt and 0 to 50% iron, and which may also contain one or more of the elements such as aluminum or titanium up to each, and molybdenum, niobium, tantalum, tungsten, vanadium, zirconium, boron and hafnium in the amounts commonly present in high temperature alloys, e.g., up to molybdenum, up to 8% of niobium and/or tantalum, up to 25% tungsten, up to 3% vanadium, up to 2% zirconium, up to 0.5 or 1% boron (preferably less than 0.1% boron), and up to 5% hafnium.
The additive may also be useful for treating melts which are refined and cast at lower temperatures, for example, melts of copper-aluminum alloys, stainless steel and other alloy steels, and brasses, e.g., 70% copper-30% zinc brass.
The following data is given as generally illustrative of the invention.
Three nickel-tungsten alloys containing 2%, 4%, and 15% tungsten, respectively, in the form of strip 0.12 mm. thick were degreased and internally oxidized by heating in air. The Ni-2%W and Ni-4%W alloys were heated at 1140C. and the Ni-l5%W alloy at 1200C. In each case the heating was continued for four hours, but with the 2% and the 4% tungsten alloys the air was removed after minutes and the heating completed in vacuum and this minimized scaling losses. The vacuum technique was unsuitable for the Ni-15%W alloy since the internal oxidation proceeded extremely slowly. The predominant composition of the additives thus prepared was Ni-3% tungsten oxide for the additive made from the alloy containing 2% tungsten, Ni-5% tungsten oxide for the additive made from the alloy containing 4% tungsten and Ni-19% tungsten oxide for the additive made from the alloy containing 15% tungsten. The average size of the oxide particles was 0.2 pm, 0.4 pm and 1.5 pm, respectively.
The oxidized strip was quenched into water, and surface oxide film removed by rubbing with emery paper, or by scratch brushing, preferably after coldrolling slightly to fracture the scale, or by pickling, for example, in hydrochloric acid.
Melts of a nickel-base superalloy (No. 1) containing, by weight, 0.09% carbon, 0.46% silicon, 0.54% iron,
An additive in the form of the strip prepared as described above and attached to a silica stirrer was introduced into melts of this alloy. The melts were poured into sythetic mullite molds (2.8 inches in diameter, 7.5 inches high, 1 inch wall thickness) preheated to 800 to 1000C. and a hot-topping compound was then added, the melts being allowed to solidify.
The extent of grain refinement was determined by comparing the as-cast structure of a transverse section of the inoculated ingots with that of a similar section taken from an untreated ingot otherwise prepared in the same fashion. The sections were taken from a position mid-way between the bottom of the shrinkage pipe and the bottom of the ingot avoiding columnar crystals grown from the bottom.
The results are set forth in Table 1.
TABLE I Tungsten Oxide The following was used to classify the ingot structures:
E medium equiaxial grain: 2.5 to 4.5 mm. diameter C,, medium columnar grain; 2.5 to 4.5 mm. diameter E coarse equiaxial grain; 4.5 to 6.0 mm. diameter C coarse columnar grain; 4.5 to 6.0 mm. diameter C very coarse columnar grain; mm. diameter It can be seen that grain refinement occured in all instances in which the nickel-tungsten oxide additives of varying oxide particle size were employed. It would appear that the extent of grain refinement is substantially independent of oxide particle size since the particle size in ingot No. 4 was 1.5 um and the results were quite satisfactory.
To illustrate that grain refinement can be obtained with the aid of tungsten oxide-containing additives over a wide range of temperatures of the melt, further tests were carried out in which Ni-5% tungsten oxide additive was added to melts of alloys having the compositions shown in Table 11.
TABLE ll COMPOSITION (Wt.
Alloy No. C Si Fe Mn Mg Cr Ti Al Ni Co Mo Nb B Zr 2 0.07 1.0 1.0 1.0 0.012 19.5 2.35 1.40 bal. 2.0 0.3 0.0025 0.06 3 0.13 1.0 1.0 1.0 15.0 1.2 4.7 bal. 20.0 5.0 0.006 0.10 4 0.05 0.35 bal. 0.35 19.0 1.0 0.6 53 1.0 3.0 5.3 0.0025 5 0.05 0.25 1.0 0.1 20.0 2.3 0.4 bal. 14.0 4.5 5.0 0.0025 0.03
19.2% chromium, 2.46% titanium, 1.5% aluminum and 16.4% cobalt, the balance being essentially nickel, were prepared in a high frequency induction furnace.
The results are reported in Table III which show that significant grain refinement was achieved in each case:
TABLE III Tungsten Oxide Pouring Proportion lngot Alloy Amount in Amount Temp. lngot of each No. No. Addmve(%) Added(- (C.) Structure grain(%) 5 2 None 1445 C,, 100 6 2 S 0.3 1445 E 100 7 3 None 1425 C, 100 8 3 5 0.3 1425 C,, E 20-80 9 4 None 1450 C,, 100 10 4 5 0.3 1450 c,,, E, 40-60 1 l 5 None 1395 C 100 12 5 5 0.3 1395 E 100 As indicated herein, a turbine wheel was integrally 15 resorted to without departing from the spirit and scope precision cast using the subject nickel-tungsten oxide nucleating additive. In this connection, the alloy used to produce the wheel was of the nickel-base superalloy type and was of the following approximate composition: 0.05%C, 11.75%Cr, 4.5%Mo, 6%Al, 0.7%Ti 2%Nb, 0.01%B, 0.1%Zr, balance nickel. The alloy was vacuum melted and cast in investment shell molds preheated to 800C. with a metal temperature of 1460C. The wheel was cut in half to show the grain size in the hub as well as the blade. The grain size was uniform throughout both sections, being less than about 1/16 inch in the hub. A similar wheel was cast without aid of the innoculant and the grain size in the hub was 'approximately A to inch, approximately 4 to 8 times larger. It has been considered that as a consequence of the fact that the blades and hubs operate under different loads and are exposed to different elevated temperatures, it would be of considerable benefit if the grain size in the hub region could be reduced, the thought being that a fine grain was more important in the hub than in the blade section.
In addition to the above information and data, the subject invention has been used to grain refine a 25%Cr-20%Ni stainless steel and an 18%Ni maraging steel. It is considered that copper base alloys can be grain refined. Superalloys containing 50% or more of nickel, from 6% to 30% chromium, up to 30% iron, aluminum in an amount of at least 0.4 or 0.5% to 8%, up to 6% titanium, e.g., 0.5 to 5% titanium, up to 8%, e.g., l to 6%, molybdenum, up to 20%, e.g., 1 to 5%, tungsten, up to 8%, e.g., 1 to 6%, niobium, up to 8%, e.g., 1 to 6%, tantalum, together with amounts of vanadium, boron, zirconium and hafnium given herein, are generally representative of other compositions deemed responsive to the invention.
As reflected by the above description, the process of the invention can be used both in the casting of ingots and in the production of castings, i.e., articles and parts made by casting. The castings may be made by investment casting in vacuum, air or an inert atmosphere, or by conventional sand casting methods.
While the oxide formed by internal oxidations of nickel-tungsten alloys is referred to in this specification as tungsten oxide, it is suspected that in practice the oxidation of such alloys may lead to additives containing some amount of nickel oxide. In-other words, a mixed oxide, for example, NiO W0 may be dispersed in the nickel carrier. Irrespective of this, the actual tungsten oxide content should preferably be from 1 or 2 to 8%.
Although the present invention has been described in conjunction with preferred embodiments, it is to be understood that modifications and variations may be of the invention, as those skilled in the art will readily understand. Such modifications and variations are considered to be within the purview and scope of the invention and appended claims.
We claim:
l. A process for grain refining a metal or alloy during solidification from the molten state which comprises introducing into a melt of the metal or alloy an in- I noculating additive comprised of a nickel carrier and tungsten oxide particles in at least a small but effective amount sufficient to induce grain refinement upon solidification, nickel dissolving in the melt and solid tungsten oxide nuclei being dispersed therein.
2. A process according to claim 1 in which the additive is in the form of strip from 0.05 to 0.4 mm. thick.
3. A process according to claim 1 in which the additive comprises an internally oxidized single-phase alloy.
4. A process according to claim 3 in which the additive comprises an internally oxidized nickel-tungsten alloy containing 1 to 17% tungsten.
5. A process according to claim 1 in which the alloy contains from 1% to 6% tungsten.
6. A process according to claim 1 in which the melt is an alloy with a base of nickel or nickel and copper or nickel and chromium or nickel, chromium and cobalt, in each case with or without iron up to 50%.
7. A process according to claim 1 in which the melt is an alloy having a composition falling within the following ranges: 20 to nickel, 5 to 35% chromium, 0 to 40% cobalt and 0 to 50% iron, up to 10% aluminum, up to 10% titanium, up to 15% molybdenum, up to 8% niobium, up to 8% tantalum, up to 25% tungsten, up to 3% vanadium, up to 2% zirconium, up to 1% boron and up to 5% hafnium.
8. A process according to claim 1 in which the melt is an alloy having a composition falling within the following ranges: from 6% to 30% chromium, up to 30% iron, aluminum in an amount of at least 0.4 to 8%, up to 6% titanium, up to 8% molybdenum, up to 20% tungsten, up to 0.25% carbon, upto 6% niobium, up to 6% tantalum, up to 3% vanadium, up to 0.5% boron, up to 2% zirconium, up to 5% hafnium, and at least about 50% nickel.
9. A process according to claim 1 in which from 0.2 to 0.8% additive by weight of the melt is introduced.
10. A process according to claim 1 in which from 0.2 to 0.5% additive by weight of the melt in introduced.
11. A process in accordance with claim 1 in which the tungsten oxide was formed by heating in air to the point that an external coating was formed and the remainder of the oxidation process was conducted in a substantial vacuum whereby scaling losses are reduced. It
Claims (11)
1. A PROCESS FOR GRAIN REFINING A METAL OR ALLOY DURING SOLIDIFICATION FROM THE MOLTEN STATE WHICH COMPRISES INTRODUCTING INTO A MELT OF THE METAL OR ALLOY AN INNOCULATING ADDITIVE COMPRISED OF A NICKEL CARRIER AND TUNGSTEN OXIDE PARTICLES IN AT LEAST A SMALL BUT EFFECTIVE AMOUNT SUFFICIENT TO INDUCE GRAIN REFINEMENT UPON SOLIDIFICATION, NICKEL DISSOLVING IN THE MELT AND SOLID TUNGSTEN OXIDE NUCLEI BEING DISPERSED THEREIN.
2. A process according to claim 1 in which the additive is in the form of strip from 0.05 to 0.4 mm. thick.
3. A process according to claim 1 in which the additive comprises an internally oxidized single-phase alloy.
4. A process according to claim 3 in which the additive comprises an internally oxidized nickel-tungsten alloy containing 1 to 17% tungsten.
5. A process according to claim 1 in which the alloy contains from 1% to 6% tungsten.
6. A process according to claim 1 in which the melt is an alloy with a base of nickel or nickel and copper or nickel and chromium or nickel, chromium and cobalt, in each case with or without iron up to 50%.
7. A process according to claim 1 in which the melt is an alloY having a composition falling within the following ranges: 20 to 80% nickel, 5 to 35% chromium, 0 to 40% cobalt and 0 to 50% iron, up to 10% aluminum, up to 10% titanium, up to 15% molybdenum, up to 8% niobium, up to 8% tantalum, up to 25% tungsten, up to 3% vanadium, up to 2% zirconium, up to 1% boron and up to 5% hafnium.
8. A process according to claim 1 in which the melt is an alloy having a composition falling within the following ranges: from 6% to 30% chromium, up to 30% iron, aluminum in an amount of at least 0.4 to 8%, up to 6% titanium, up to 8% molybdenum, up to 20% tungsten, up to 0.25% carbon, up to 6% niobium, up to 6% tantalum, up to 3% vanadium, up to 0.5% boron, up to 2% zirconium, up to 5% hafnium, and at least about 50% nickel.
9. A process according to claim 1 in which from 0.2 to 0.8% additive by weight of the melt is introduced.
10. A process according to claim 1 in which from 0.2 to 0.5% additive by weight of the melt in introduced.
11. A process in accordance with claim 1 in which the tungsten oxide was formed by heating in air to the point that an external coating was formed and the remainder of the oxidation process was conducted in a substantial vacuum whereby scaling losses are reduced.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US362521A US3929467A (en) | 1973-05-21 | 1973-05-21 | Grain refining of metals and alloys |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US362521A US3929467A (en) | 1973-05-21 | 1973-05-21 | Grain refining of metals and alloys |
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| US3929467A true US3929467A (en) | 1975-12-30 |
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| US362521A Expired - Lifetime US3929467A (en) | 1973-05-21 | 1973-05-21 | Grain refining of metals and alloys |
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| US (1) | US3929467A (en) |
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| US4111685A (en) * | 1976-11-04 | 1978-09-05 | Special Metals Corporation | Dispersion-strengthened cobalt-bearing metal |
| WO1985003019A1 (en) * | 1984-01-12 | 1985-07-18 | Demetron, Inc. | Method and apparatus for high vacuum casting |
| US6360936B1 (en) * | 1999-05-11 | 2002-03-26 | Aktiengesellschaft der Dillinger Hüttenwerke | Method of manufacturing a composite sheet steel, especially for the protection of vehicles against shots |
| US20030010554A1 (en) * | 2000-01-31 | 2003-01-16 | Oystein Grong | System for balancing a two-wheeled vehicle at rest |
| US20070084754A1 (en) * | 2004-09-22 | 2007-04-19 | Soled Stuart L | Bulk bimetallic catalysts, method of making bulk bimetallic catalysts and hydroprocessing using bulk bimetallic catalysts |
| US20100028197A1 (en) * | 2006-09-21 | 2010-02-04 | Mark Heazle | Nickel-based alloys and articles made therefrom |
| US20100080729A1 (en) * | 2006-06-02 | 2010-04-01 | Power Systems Manufacturing, Llc | Nickel-base alloy for gas turbine applications |
| RU2562202C1 (en) * | 2014-06-11 | 2015-09-10 | Открытое акционерное общество Научно-производственное объединение "Центральный научно-исследовательский институт технологии машиностроения" ОАО НПО "ЦНИИТМАШ" | Composition of nickel-based heat-resistant alloy charge of equiaxial structure for gas turbine working blade casting |
| US9828658B2 (en) | 2013-08-13 | 2017-11-28 | Rolls-Royce Corporation | Composite niobium-bearing superalloys |
| US9938610B2 (en) | 2013-09-20 | 2018-04-10 | Rolls-Royce Corporation | High temperature niobium-bearing superalloys |
| DE102018208737A1 (en) * | 2018-06-04 | 2019-12-05 | Siemens Aktiengesellschaft | Y, Y` hardened cobalt-nickel base alloy, powder, component and process |
| DE102018208736A1 (en) * | 2018-06-04 | 2019-12-05 | Siemens Aktiengesellschaft | Y, Y 'hardened cobalt-nickel base alloy, powder, component and process |
| CN110872652A (en) * | 2018-08-29 | 2020-03-10 | 中国科学院金属研究所 | A kind of preparation method and application of superalloy internal grain refiner |
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| US9938610B2 (en) | 2013-09-20 | 2018-04-10 | Rolls-Royce Corporation | High temperature niobium-bearing superalloys |
| RU2562202C1 (en) * | 2014-06-11 | 2015-09-10 | Открытое акционерное общество Научно-производственное объединение "Центральный научно-исследовательский институт технологии машиностроения" ОАО НПО "ЦНИИТМАШ" | Composition of nickel-based heat-resistant alloy charge of equiaxial structure for gas turbine working blade casting |
| DE102018208737A1 (en) * | 2018-06-04 | 2019-12-05 | Siemens Aktiengesellschaft | Y, Y` hardened cobalt-nickel base alloy, powder, component and process |
| DE102018208736A1 (en) * | 2018-06-04 | 2019-12-05 | Siemens Aktiengesellschaft | Y, Y 'hardened cobalt-nickel base alloy, powder, component and process |
| CN110872652A (en) * | 2018-08-29 | 2020-03-10 | 中国科学院金属研究所 | A kind of preparation method and application of superalloy internal grain refiner |
| CN110872652B (en) * | 2018-08-29 | 2021-09-24 | 中国科学院金属研究所 | A kind of preparation method and application of superalloy internal grain refiner |
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